WO2005072233A3 - Aeronef a decollage et a atterrissage verticaux silencieux faisant intervenir des rotors a impulsion d'air carenes a induction magnetique - Google Patents

Aeronef a decollage et a atterrissage verticaux silencieux faisant intervenir des rotors a impulsion d'air carenes a induction magnetique Download PDF

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Publication number
WO2005072233A3
WO2005072233A3 PCT/US2005/001835 US2005001835W WO2005072233A3 WO 2005072233 A3 WO2005072233 A3 WO 2005072233A3 US 2005001835 W US2005001835 W US 2005001835W WO 2005072233 A3 WO2005072233 A3 WO 2005072233A3
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WO
WIPO (PCT)
Prior art keywords
air
aircraft
impeller
engine
magnetic induction
Prior art date
Application number
PCT/US2005/001835
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English (en)
Other versions
WO2005072233A2 (fr
Inventor
John K Sanders Jr
J Kenneth Sanders
Arturo Aviles Jr
Arturo F Aviles
Original Assignee
Ufoz Llc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ufoz Llc filed Critical Ufoz Llc
Publication of WO2005072233A2 publication Critical patent/WO2005072233A2/fr
Publication of WO2005072233A3 publication Critical patent/WO2005072233A3/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/20—Vertical take-off and landing [VTOL] aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/24—Coaxial rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/60—UAVs characterised by the material
    • B64U20/65—Composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Details Of Aerials (AREA)

Abstract

Selon l'invention, un aéronef de vol stationnaire utilise un moteur à impulsion d'air qui comprend un conduit de passage d'air et un rotor dont les extrémités extérieures des pales sont fixées à un disque d'impulsion annulaire entraîné par des éléments à induction magnétique disposés en réseau dans le conduit de passage d'air. Le moteur à impulsion d'air est disposé verticalement dans le corps de l'aéronef afin de produire une poussée verticale pour le décollage et l'atterrissage verticaux. De préférence, le moteur à impulsion d'air utilise des rotors doubles, coaxiaux, contra-rotatifs destinés à assurer une poussée et une stabilité gyroscopique améliorées. Un ensemble ailette d'air dirige une partie de l'air de poussée émis à un angle désiré afin d'obtenir une composante de poussée horizontale pour les manoeuvres de vol ou les mouvements de déplacement. L'aéronef peut utiliser un seul moteur dans un fuselage annulaire, deux moteurs sur un châssis de fuselage longitudinal, trois moteurs dans un agencement triangulaire pour une stabilité de vol vers l'avant, ou d'autres agencements à moteurs multiples dans une configuration équilibrée, symétrique. D'autre mécanismes de commande de vol peuvent être utilisés, notamment des ailettes marginales latérales, une aile verticale, et/ou des gouvernes de direction ou des volets hypersustentateurs. Un système de commande de vol intégré peut être utilisé afin d'activer les divers mécanismes de commande de vol. Le courant électrique est fourni aux propulseurs à induction magnétique par des batteries légères ou des piles à combustibles à haute capacité. Ledit aéronef de vol stationnaire est particulièrement apte à être utilisé dans des applications faisant appel à la fonction VTOL, dans des opérations de vol stationnaire pour une surveillance silencieuse, pour les manoeuvres dans des espaces aériens fermés, et pour des vols de longue durée destinés à assurer une surveillance continue de cibles terrestres et d'installations importantes nécessitant une surveillance constante.
PCT/US2005/001835 2004-01-22 2005-01-19 Aeronef a decollage et a atterrissage verticaux silencieux faisant intervenir des rotors a impulsion d'air carenes a induction magnetique WO2005072233A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/763,973 2004-01-22
US10/763,973 US7032861B2 (en) 2002-01-07 2004-01-22 Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors

Publications (2)

Publication Number Publication Date
WO2005072233A2 WO2005072233A2 (fr) 2005-08-11
WO2005072233A3 true WO2005072233A3 (fr) 2005-12-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/001835 WO2005072233A2 (fr) 2004-01-22 2005-01-19 Aeronef a decollage et a atterrissage verticaux silencieux faisant intervenir des rotors a impulsion d'air carenes a induction magnetique

Country Status (2)

Country Link
US (2) US7032861B2 (fr)
WO (1) WO2005072233A2 (fr)

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US20070034738A1 (en) 2007-02-15
WO2005072233A2 (fr) 2005-08-11
US20060049304A1 (en) 2006-03-09
US7032861B2 (en) 2006-04-25
US7249732B2 (en) 2007-07-31

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